Special take off technique required. No. A No. A. 2. Landing. A. Special landing technique required. No. A No. A. 3. Speed in straight flight. B. Trim speed more ...
Flight test report: EN 926-2:2013 & LTF 91/09 Manufacturer
Dudek Paragliders S.J.
Certification number
PG_1130.2016
Address
ul. Centralna 2U 86-031 Osielsko Poland
Date of flight test
13. 12. 2016
Glider model
Colt 2 27
Classification
C
Serial number
P-143341
Representative
None
Trimmer
no
Place of test
Villeneuve
Folding lines used
no
Test pilot
Thurnheer Claude
Zoller Alain
Harness
Niviuk - Gingo 2 M
Gin Gliders - Gingo 2 L
Harness to risers distance (cm)
44
44
Distance between risers (cm)
44
46
Total weight in flight (kg)
95
120
1. Inflation/Take-off
B
Rising behaviour
Easy rising, some pilot correction is required
B
Easy rising, some pilot correction is required
B
Special take off technique required
No
A
No
A
2. Landing
A
Special landing technique required
No
A
No
A
3. Speed in straight flight
B
Trim speed more than 30 km/h
Yes
A
Yes
A
Speed range using the controls larger than 10 km/h
Yes
A
Yes
A
Minimum speed
25 km/h to 30 km/h
B
Less than 25 km/h
A
4. Control movement
A
not available
0
not available
0
Increasing / greater than 60 cm
A
not available
0
Symmetric control pressure / travel
not available
0
Increasing / greater than 65 cm
A
5. Pitch stability exiting accelerated flight
A
Dive forward angle on exit
Dive forward less than 30°
A
Dive forward less than 30°
A
Collapse occurs
No
A
No
A
6. Pitch stability operating controls during accelerated flight
A
Collapse occurs
No
A
No
A
7. Roll stability and damping
A
Oscillations
Reducing
A
Reducing
A
8. Stability in gentle spirals
A
Tendency to return to straight flight
Spontaneous exit
A
Spontaneous exit
A
9. Behaviour exiting a fully developed spiral dive
C
Initial response of glider (first 180°)
Immediate reduction of rate of turn
A
No immediate reaction
B
Tendency to return to straight flight
Spontaneous exit (g force decreasing, rate of turn decreasing)
A
Spontaneous exit (g force decreasing, rate of turn decreasing)
A
Max. weight in flight up to 80 kg Symmetric control pressure / travel Max. weight in flight 80 kg to 100 kg Symmetric control pressure / travel Max. weight in flight greater than 100 kg
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Turn angle to recover normal flight
Less than 720°, spontaneous recovery
10. Symmetric front collapse
B
A
1080° to 1440°, spontaneous recovery
C
Approximately 30 % chord Entry
Rocking back less than 45°
A
Rocking back less than 45°
A
Recovery
Spontaneous in 3 s to 5 s
B
Spontaneous in 3 s to 5 s
B
Dive forward angle on exit Change of course
Dive forward 0° to 30° Keeping course
A
Dive forward 0° to 30° Keeping course
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
At least 50% chord Entry
Rocking back less than 45°
A
Rocking back less than 45°
A
Recovery
Spontaneous in 3 s to 5 s
B
Spontaneous in 3 s to 5 s
B
Dive forward angle on exit / Change of course
Dive forward 0° to 30° / Keeping course
A
Dive forward 0° to 30° / Keeping course
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
With accelerator Entry
Rocking back less than 45°
A
Rocking back less than 45°
A
Recovery
Spontaneous in 3 s to 5 s
B
Spontaneous in 3 s to 5 s
B
Dive forward angle on exit / Change of course
Dive forward 0° to 30° / Keeping course
A
Dive forward 30° to 60° / Keeping course
B
Cascade occurs
No
A
No
A
Folding lines used
No
11. Exiting deep stall (parachutal stall)
A
Deep stall achieved
Yes
A
Yes
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Change of course
Changing course less than 45°
A
Changing course less than 45°
A
Cascade occurs
No
A
No
A
12. High angle of attack recovery
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Cascade occurs
No
A
No
A
13. Recovery from a developed full stall
B
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 30° to 60°
B
Collapse
No collapse
A
No collapse
A
Cascade occurs (other than collapses)
No
A
No
A
Rocking back
Less than 45°
A
Less than 45°
A
Line tension
Most lines tight
A
Most lines tight
A
14. Asymmetric collapse
C
No
Small asymmetric collapse Change of course until re-inflation / Maximum dive forward or roll angle
Less than 90° / Dive or roll angle 0° to 15°
A
Less than 90° / Dive or roll angle 0° to 15°
A
Re-inflation behaviour
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
Large asymmetric collapse Change of course until re-inflation / Maximum dive forward or roll angle
90° to 180° / Dive or roll angle 15° to 45°
B
90° to 180° / Dive or roll angle 45° to 60°
C
Re-inflation behaviour
Inflates in less than 3 s from start of pilot action
C
Spontaneous re-inflation
A
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Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
Small asymmetric collapse with fully activated accelerator Change of course until re-inflation / Maximum dive forward or roll angle
Less than 90° / Dive or roll angle 15° to 45°
A
Less than 90° / Dive or roll angle 15° to 45°
A
Re-inflation behaviour
Spontaneous re-inflation
A
Spontaneous re-inflation
A
Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
No
Large asymmetric collapse with fully activated accelerator Change of course until re-inflation / Maximum dive forward or roll angle
Less than 90° / Dive or roll angle 45° to 60°
C
90° to 180° / Dive or roll angle 45° to 60°
C
Re-inflation behaviour
Spontaneous re-inflation
A
Inflates in less than 3 s from start of pilot action
C
Total change of course
Less than 360°
A
Less than 360°
A
Collapse on the opposite side occurs
No (or only a small number of collapsed cells with a spontaneous reinflation)
A
Yes, no turn reversal
C
Twist occurs
No
A
No
A
Cascade occurs
No
A
No
A
Folding lines used
No
15. Directional control with a maintained asymmetric collapse
A
Able to keep course
Yes
A
Yes
A
180° turn away from the collapsed side possible in 10 s
Yes
A
Yes
A
Amount of control range between turn and stall or spin
More than 50 % of the symmetric control travel
A
More than 50 % of the symmetric control travel
A
16. Trim speed spin tendency
A
Spin occurs
No
A
No
A
17. Low speed spin tendency
A
Spin occurs
No
A
No
A
18. Recovery from a developed spin
B
Spin rotation angle after release
Stops spinning in less than 90°
A
Stops spinning in 90° to 180°
B
Cascade occurs
No
A
No
A
19. B-line stall
A
Change of course before release
Changing course less than 45°
A
Changing course less than 45°
A
Behaviour before release
Remains stable with straight span
A
Remains stable with straight span
A
Recovery
Spontaneous in less than 3 s
A
Spontaneous in less than 3 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Cascade occurs
No
A
No
A
20. Big ears
B
Entry procedure
Dedicated controls
A
Dedicated controls
A
Behaviour during big ears
Stable flight
A
Stable flight
A
Recovery
Spontaneous in 3 s to 5 s
B
Spontaneous in less than 3 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
21. Big ears in accelerated flight
B
Entry procedure
Dedicated controls
A
Dedicated controls
A
Behaviour during big ears
Stable flight
A
Stable flight
A
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No
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Recovery
Recovery through pilot action in less than a further 3 s
B
Spontaneous in 3 s to 5 s
A
Dive forward angle on exit
Dive forward 0° to 30°
A
Dive forward 0° to 30°
A
Behaviour immediately after releasing the accelerator while maintaining big ears
Stable flight
A
Stable flight
A
22. Alternative means of directional control
A
180° turn achievable in 20 s
Yes
A
Yes
A
Stall or spin occurs
No
A
No
A
23. Any other flight procedure and/or configuration described in the user's manual
0
Procedure works as described
not available
0
not available
0
Procedure suitable for novice pilots
not available
0
not available
0
Cascade occurs
not available
0
not available
0
24. Comments of test pilot Comments
Test Report generated automatically by AIR TURQUOISE SA, valid without signature
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